Basic Information

Category Fixed Wing Type Unmanned Aerial Vehicle (UAV)
Year Commissioned 2006 Year Decommissioned 0
Agility 0.5 Damage Points (DP) 3
Empty Weight 150 kg Max Weight 161 kg
Runway Information Catapult Launcher Physical Size UAS [NATO Class I, Small] (20-150kg)
Cost 0 Hypothetical No
Payload Weight 0 kg Crew 0 people

Aircraft Capabilities

Night Navigation (Ferry, Air-to-Air, Air-to-Surface Missiles)

Sensor Parameters

Model Purpose Range Scan Interval Generation
WBG 96 Infrared, Surveillance Camera 0.00 - 30.00 nm 10 sec Infrared, 3rd Generation Imaging (2000s/2010s, Impr LANTIRN, Litening II/III, ATFLIR)

Sensor Coverage Diagram
Model Detection Angle Omnidirectional
WBG 96 SB1, SB2, SMF1, SMF2, SMA1, SMA2, SS1, SS2, PB1, PB2, PMF1, PMF2, PMA1, PMA2, PS1, PS2

Weapon Loadouts Click to Expand Beta

Loadout Type Role Ready Time Combat Radius
No Data
No Data
No Data
No Data

Signatures

Type Front Side Rear
Visual Detection Range 0.67 nm 1.09 nm 0.67 nm
Visual Classification Range 0.48 nm 0.82 nm 0.62 nm
Infrared Detection Range 0.67 nm 2.5 nm 7.36 nm
Infrared Classification Range 0.48 nm 0.82 nm 0.48 nm
Radar, A-D Band (30-2000 MHz) -11.3 dBsm (0.0741 m²) -8.3 dBsm (0.1479 m²) -11.3 dBsm (0.0741 m²)
Radar, E-M Band (2-100 GHz) -11.3 dBsm (0.0741 m²) -8.3 dBsm (0.1479 m²) -11.3 dBsm (0.0741 m²)

Default Configuration

Model Comments
No Data

Datalink

Type Model Range Channels
Radio UHF/VHF Radio [Unsecure] 100 nm 0

Engines

Model Type Engine Count Military Thrust Afterburner Thrust Military Fuel Rate (SFC) Afterburner Fuel Rate (SFC) Hypothetical Comments
1x ZF Sachs Piston Piston 1 33 - 1.25 - No -

Fuel

Fuel Type Fuel Capacity
Aviation Fuel 65